# N859FD: 2013 Boeing 777-FS2

- Status: Valid registration
- Airframe: [Boeing 777-FS2](https://openairdocs.org/model/boeing-777-fs2) (registry code 138527H, 13 seats)
- Engine: [GE GE90-110B1](https://openairdocs.org/engine/ge-ge90-110b1) (registry code 30046)
- Data sheets: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (General Electric Company GE Aviation) (OpenAirDocs)
- Serial number: 37730
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 13, 2013
- Certificate issued: September 13, 2013
- Expires: September 30, 2029
- Mode S code: ABC948
- Registered owner: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=859FD
- Page: https://openairdocs.org/aircraft/N859FD

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 21 in force

### Matched by airframe (Boeing 777-FS2)

None in force.

### Matched by engine (GE GE90-110B1)

- [AD 2025-25-07](https://openairdocs.org/ad/2025-25-07): Turbine Section · General Electric Company GE GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 6, 2026
- [AD 2025-07-10](https://openairdocs.org/ad/2025-07-10): Fuel Controlling System · General Electric Company GE GE90-110B1 and GE90-115B. Effective May 21, 2025
- [AD 2024-06-15](https://openairdocs.org/ad/2024-06-15): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 14, 2024
- [AD 2023-26-07](https://openairdocs.org/ad/2023-26-07): Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 27, 2024
- [AD 2023-04-19](https://openairdocs.org/ad/2023-04-19): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 27, 2023
- [AD 2022-23-09](https://openairdocs.org/ad/2022-23-09): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Jan 17, 2023
- [AD 2022-18-06](https://openairdocs.org/ad/2022-18-06): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 26, 2022
- [AD 2021-26-06](https://openairdocs.org/ad/2021-26-06): Turbine Engine Accessory Drive · General Electric GE90-76B, GE90-85B, GE90-90B and 3 more. Effective Feb 15, 2022
- [AD 2020-21-13](https://openairdocs.org/ad/2020-21-13): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 17, 2020
- [AD 2020-18-14](https://openairdocs.org/ad/2020-18-14): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Oct 21, 2020
- [AD 2020-10-04](https://openairdocs.org/ad/2020-10-04): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 27, 2020
- [AD 2020-01-55](https://openairdocs.org/ad/2020-01-55): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 2, 2020
- [AD 2018-20-23](https://openairdocs.org/ad/2018-20-23): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 30, 2018
- [AD 2018-20-22](https://openairdocs.org/ad/2018-20-22): Turbine Section · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Nov 13, 2018
- [AD 2017-08-06](https://openairdocs.org/ad/2017-08-06): Engine Oil Cooler · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective May 22, 2017
- [AD 2013-23-18](https://openairdocs.org/ad/2013-23-18): Variable bypass valve (VBV) actuator fuel supply tube · General Electric GE90-110B1 and GE90-115B. Effective Jan 7, 2014
- [AD 2013-17-07](https://openairdocs.org/ad/2013-17-07): Stage 1 high-pressure turbine (HPT) stator shrouds · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 18, 2013
- [AD 2013-15-20](https://openairdocs.org/ad/2013-15-20): Transfer gearbox assembly (TGB) radial gearshafts · General Electric GE90-110B1, GE90-113B, GE90-115B and 5 more. Effective Aug 21, 2013
- [AD 2011-26-11](https://openairdocs.org/ad/2011-26-11): HPC stages 1-2 seal teeth · General Electric GE90-110B1 and GE90-115B. Effective Feb 3, 2012
- [AD 2009-25-14](https://openairdocs.org/ad/2009-25-14): Blade · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jan 19, 2010
- [AD 2007-10-05](https://openairdocs.org/ad/2007-10-05): Turbine Center Frames (TCFs) · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jun 14, 2007

### Historical (superseded or no longer in force)

- [AD 2021-15-05](https://openairdocs.org/ad/2021-15-05) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Sep 13, 2021
- [AD 2020-20-17](https://openairdocs.org/ad/2020-20-17) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Oct 23, 2020
- [AD 2017-07-04](https://openairdocs.org/ad/2017-07-04) (historical): Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Apr 21, 2017
- [AD 2013-24-17](https://openairdocs.org/ad/2013-24-17) (historical): High pressure compressor (HPC) rotor stage 2-5 spools · General Electric GE90-110B1 and GE90-115B. Effective Dec 31, 2013
- [AD 2013-14-51](https://openairdocs.org/ad/2013-14-51) (historical): Failure of a transfer gearbox assembly radial gearshaft · General Electric GE90-110B1 and GE90-115B
- [AD 2013-10-52](https://openairdocs.org/ad/2013-10-52) (historical): Transfer gearbox assemblies (TGBs) · General Electric GE90-110B1 and GE90-115B. Effective Jun 26, 2013

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N859FD.

## FAA accident and incident reports

None matched to N859FD.

## Service difficulty reports (19)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR FDEA202606110701](https://openairdocs.org/sdr/FDEA202606110701), Jun 11, 2026: SKIN. DELAMINATED. LHW OB FLAP LWR SURFACE 265IN FROM IB EDGE, 10IN FROM LWR EDGE FOUND DELAMINATION. REPAIRED LHW OB FLAP LWR SURFACE DELAMINATION AT OTEF STA 281 AS PER B777 SRM
- [SDR FDEA202606090690](https://openairdocs.org/sdr/FDEA202606090690), Jun 9, 2026: RETAINER. DAMAGED. FOUND RH WING SLAT NR 8 IB EDGE SEAL RETAINER UPPER SURFACE AFT SECOND FASTENER HOLE WORN. RH WING NO.8 SLAT IB EDGE OUTER SKIN FASTENER HOLE WORN AREA REPAIRED
- [SDR FDEA202606090689](https://openairdocs.org/sdr/FDEA202606090689), Jun 9, 2026: SKIN. DAMAGED. NO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE FOUND WORN. NO.7 SLAT EXTERNAL UPPER SURFACE OUTER SKIN AT ISS 184 SCREW HOLE WORN AREA REPAIR
- [SDR FDEA202606060678](https://openairdocs.org/sdr/FDEA202606060678), Jun 6, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD: E G-5710-E0376285 G P11 STEP 5.A.(2) THEN FOUND 01 EA CRACKED ON LT UPPER WING SKIN FASTENER NR 5. REPAIRED AS PER B777 SRM 51-40-05- 
- [SDR FDEA202606060677](https://openairdocs.org/sdr/FDEA202606060677), Jun 6, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:E G-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 01 EA CRACK ON RH UPPER WING SKIN FASTENER #5. REPAIRED AS PER B777 SRM 51-40-05- 0G FI
- [SDR FDEA202606050673](https://openairdocs.org/sdr/FDEA202606050673), Jun 5, 2026: SKIN. DAMAGED. REQUEST A PERMANENT REPAIR ON AFT FUSELAGE SKIN STA 2319 TO STA 2344.5, S-48R TO S-49R.
- [SDR FDEA202602180233](https://openairdocs.org/sdr/FDEA202602180233), Feb 18, 2026: SLIDE. DAMAGED. R1 DOOR SLIDE REQUIRES CORRECT BREAKAWAY WIRE TO BE INSTALLED ON PACKBOARD RELEASE CABLE. REF F.E.A. G2560-F0386294 C P1. INSTALLED CAD-PLATED COPPER BREAKAWAY 
- [SDR FDEA202309051545](https://openairdocs.org/sdr/FDEA202309051545), Sep 5, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 FOUND CRACKED AT STA1706 RBL1 EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 AT STA 1706 RBL 1 CRACK SIZE L=3.5
- [SDR FDEA202309051544](https://openairdocs.org/sdr/FDEA202309051544), Sep 5, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND CRACKED AT STA1660 RBL1. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 AT STA 1660 RBL 1 CRACK SIZE L=3.
- [SDR FDEA202106101495](https://openairdocs.org/sdr/FDEA202106101495), Jun 10, 2021: BRAKE ASSY. BURNED. MDIS 859 32-40 8127 10JUN21 CDG FACT U AT ARRIVAL, #1 BRAKE FIRE. MAX VALUES: #1 WHEEL/BRAKE: 265PSI TEMP:4.4 #2 WHEEL/BRAKE: 270PSI 4.3 #3 WHEEL/BRAKE: 250PSI 
- [SDR FDEA202106101494](https://openairdocs.org/sdr/FDEA202106101494), Jun 10, 2021: BRAKE ASSY. FIRE. MDIS 859 32-40 8127 10JUN21 CDG AT ARRIVAL, #1 BRAKE FIRE. MAX VALUES: #1 WHEEL/BRAKE: 265PSI TEMP:4.4 #2 WHEEL/BRAKE: 270PSI 4.3 #3 WHEEL/BRAKE: 250PSI 1.8 #4 
- [SDR FDEA2020052211028](https://openairdocs.org/sdr/FDEA2020052211028), May 21, 2020: PSEU. LOOSE. NUMEROUS STATUS MESSAGES RELATED TO EICAS CAUTION AUTOSPEED BRAKES. PSEU 2, PSEU 1, GEAR CONTROL...AND MANY MORE. ALL CAME ON WHEN CAUTION CAME UP. FOUND PSEU #
- [SDR FDEA201902210470](https://openairdocs.org/sdr/FDEA201902210470), Feb 21, 2019: LIGHT. INOPERATIVE. POST-FLT INSP, ONE OVRHD LT INOP ON EMERGENCY LT'S TEST. RE-LAMPED, REF AMM 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.
- [SDR FDEA201902190452](https://openairdocs.org/sdr/FDEA201902190452), Feb 19, 2019: WINDOW. DIRTY. DOOR 1L FORWARD WINDOW FOR GIRT BAR FLAG ON RIGHT SIDE (NOSE) SIDE DOES NOT FULLY SHOW YELLOW FLAG IN THE WINDOW WHEN 1L DOOR ARMED. DIFFICULT TO TELL IN THAT W
- [SDR FDEA2018092532658](https://openairdocs.org/sdr/FDEA2018092532658), Sep 23, 2018: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT STA 1932, RBL 36 FLOOR SUPPORT FOUND CRACK. REPAIRED AS PER SRM 53-70-53-2R FIG 202 REPAIR 2 FROM STATION 1925 TO STATION 1968 RBL 
- [SDR FDEA201711083189](https://openairdocs.org/sdr/FDEA201711083189), Nov 8, 2017: COVER. BROKEN. 1R ENTRY DOOR, SIDE EXIT LIGHT COVER BROKEN OFF. REMOVED AND REPLACED BROKEN EMERGENCY EXIT LIGHT IAW AMM 33-51-01-2. OPS CHECKED GOOD AT THIS TIME. A/C OK FOR 
- [SDR FDEA201706281780](https://openairdocs.org/sdr/FDEA201706281780), Jun 28, 2017: DOOR. OUT OF ADJUST. L1 DOOR HARD TO ARM AND ONCE ARMED, RAMP AGENT INFORMED CREW THAT THE DOOR DID NOT APPEAR CLOSED. PREFORMED PASSANGER DOOR ENTRY ADJUSTMENT AND TEST IAW AMM 52-
- [SDR FDEA201608283063](https://openairdocs.org/sdr/FDEA201608283063), Aug 28, 2016: APU. SMOKE. APU OIL QTY STATUS MESSAGE FOLLOWED BY SMOKE IN THE COCKPIT. PERFORMED AIR CONDITIONING SYSTEM OIL CONTAMINATION REMOVAL IAW AMM 21-00-01-2, AND AMM 05-51-50-2.
- [SDR FDEA201401070065](https://openairdocs.org/sdr/FDEA201401070065), Jan 7, 2014: GUARD. BROKEN. PER CREW DEBRIEF EMERGENCY LIGHTS SWITCH GUARD BROKEN. GUARD SPRING IS BROKEN, SWITCH WORKS OK. REPLACED SWITCH GUARD IAW SMP.

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 777-FS2 aircraft: https://openairdocs.org/model/boeing-777-fs2/aircraft.md
- The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.